View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 50825U 26145.51912757 +.00000000 +00000-0 +13000-3 0 00005
2 50825 53.2101 184.2198 0000959 71.5747 288.5349 15.08831961 02
| Epoch (UTC): | 25 May 2026 12:27:32 |
| Eccentricity: | 0.0000959 |
| inclination: | 53.2101° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 184.2198° |
| argument of perigee: | 71.5747° |
| revolutions per day: | 15.08831961 |
| mean anomaly at epoch: | 288.5349° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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